SAE AS1650A PDF
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Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification
Description
This aerospace specification defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -65 to +400 °F and at 125 psig nominal operating pressure.
History
| AS1650F | 2018-10-24 | Latest | Revised |
| AS1650E | 2017-12-07 | Historical | Revised |
| AS1650D | 2017-07-10 | Historical | Revised |
| AS1650C | 2016-02-26 | Historical | Revised |
| AS1650B | 2010-08-24 | Historical | Revised |
| AS1650A | 2005-06-02 | Historical | Reaffirmed |
| AS1650 | 1998-03-01 | Historical | Reaffirmed |
| ISSUING COMMITTEE | G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies |
|---|---|
| DATE | 2005-06-02 |
| DOI | |
| ISCURRENT | |
| PAGE | 29 |
| PUBLISHER | SAE International |
| REVISED | REAFFIRMED |
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